[list_settings.list_name] Current ISS TLEs @ 06:30 UTC

 
Date: December 5th 2018

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 17659 2714 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 70 5 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 049 ET - UTC (sec) : 68 18 UT1 - UTC (sec) : 0 00

Maneuvers contained within the current ephemeris are as follows:

IMPULSIVE TIG (GMT) M50 DVx(FPS) LVLH DVx(FPS) DVmag(FPS) IMPULSIVE TIG (MET) M50 DVy(FPS) LVLH DVy(FPS) Invar Sph HA DT M50 DVz(FPS) LVLH DVz(FPS) Invar Sph HP


339/18:16:16 000 0 0 0 0 0 0
N/A 0 0 0 0 223 0
000/00:00:00 000 0 0 0 0 212 9

341/20:20:00 000 0 0 0 0 0 0
N/A 0 0 0 0 222 8
000/00:00:00 000 0 0 0 0 213 1

344/23:07:30 000 0 0 0 0 0 0
N/A 0 0 0 0 222 7
000/00:00:00 000 0 0 0 0 213 4

348/03:56:00 000 0 0 0 0 0 0
N/A 0 0 0 0 222 4
000/00:00:00 000 0 0 0 0 213 6

354/01:40:30 000 0 0 0 0 0 0
N/A 0 0 0 0 222 1
000/00:00:00 000 0 0 0 0 214 1

Coasting Arc #1 (Orbit 2514)
---------------------------------------

Vector Time (GMT): 2018/339/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 944383
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         156541
05                 A    =         6785426
03  meter
 Y    =        6025750
74  meter          E    =           
0009565
 Z    =       -3119905
92                 I    =           51
30225
 XDOT =      -5457
180083                 Wp   =          108
87702
 YDOT =      -2354
254332  meter/sec      RA   =          244
01569  deg
 ZDOT =      -4836
029025                 TA   =          107
20701
                                          MA   =          107
10228
                                          Ha   =            222
899  n
mi
                                          Hp   =            213
028

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =         513586
11                 X    =          104302
90
 Y    =       19769523
43  feet           Y    =         6027209
47  meter
 Z    =      -10235911
81                 Z    =        -3119271
87
 XDOT =     -17904
134129                 XDOT =       -5406
957276
 YDOT =      -7723
931534  feet/sec       YDOT =       -2414
999103  meter/sec
 ZDOT =     -15866
236960                 ZDOT =       -4862
416785

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -19107292
52                 X    =        -5823902
76
 Y    =       -5104277
83  feet           Y    =        -1555783
88  meter
 Z    =      -10233740
20                 Z    =        -3119244
01
 XDOT =      12126
602780                 XDOT =        3696
188527
 YDOT =     -13446
678529  feet/sec       YDOT =       -4098
547616  meter/sec
 ZDOT =     -15984
635389                 ZDOT =       -4872
116867


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   18339
52579699  
00016717  00000-0  10270-3 0  9003
2 25544  51
6415 244
8758 0005068 112
4832 247
6857 15
54051712 25155


Satellite: ISS
Catalog Number: 25544
Epoch time:      18339
52579699   =   yrday
fracday
Element set:     900
Inclination:       51
6415  deg
RA of node:       244
8758  deg
Eccentricity:     
0005068     
Arg of perigee:   112
4832  deg
Mean anomaly:     247
6857  deg
Mean motion:   15
54051712  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2515
Checksum:              332


Coasting Arc #2 (Orbit 2518)
---------------------------------------

Vector Time (GMT): 2018/339/18:16:16
000
Vector Time (MET): N/A
Weight (LBS)     : 944383
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1620772
87                 A    =         6780777
42  meter
 Y    =        4785491
63  meter          E    =           
0014103
 Z    =       -4535078
08                 I    =           51
28668
 XDOT =      -5207
243755                 Wp   =           85
64206
 YDOT =      -4686
477615  meter/sec      RA   =          242
70157  deg
 ZDOT =      -3091
545079                 TA   =          153
23530
                                          MA   =          153
16246
                                          Ha   =            222
960  n
mi
                                          Hp   =            212
888

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -5317496
31                 X    =        -1652135
73
 Y    =       15700431
87  feet           Y    =         4767192
06  meter
 Z    =      -14878865
10                 Z    =        -4543027
13
 XDOT =     -17084
133055                 XDOT =       -5139
433886
 YDOT =     -15375
582727  feet/sec       YDOT =       -4744
329215  meter/sec
 ZDOT =     -10142
864434                 ZDOT =       -3116
676206

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -8447364
85                 X    =        -2574756
80
 Y    =       14224635
78  feet           Y    =         4335668
99  meter
 Z    =      -14915150
63                 Z    =        -4546137
91
 XDOT =     -12306
745206                 XDOT =       -3751
095939
 YDOT =     -18036
586063  feet/sec       YDOT =       -5497
551432  meter/sec
 ZDOT =     -10255
353193                 ZDOT =       -3125
831653


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   18339
78301784  
00016717  00000-0  10270-3 0  9010
2 25544  51
6375 243
5899 0005359 115
3021 244
8687 15
54063064 25194


Satellite: ISS
Catalog Number: 25544
Epoch time:      18339
78301784   =   yrday
fracday
Element set:     901
Inclination:       51
6375  deg
RA of node:       243
5899  deg
Eccentricity:     
0005359     
Arg of perigee:   115
3021  deg
Mean anomaly:     244
8687  deg
Mean motion:   15
54063064  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2519
Checksum:              328


Coasting Arc #3 (Orbit 2534)
---------------------------------------

Vector Time (GMT): 2018/340/18:16:16
000
Vector Time (MET): N/A
Weight (LBS)     : 944383
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2677232
90                 A    =         6778271
66  meter
 Y    =       -3489627
88  meter          E    =           
0009679
 Z    =        5151421
70                 I    =           51
29287
 XDOT =       4904
763009                 Wp   =          122
20532
 YDOT =       5748
010143  meter/sec      RA   =          237
68244  deg
 ZDOT =       1337
801174                 TA   =          314
84623
                                          MA   =          314
92483
                                          Ha   =            222
888  n
mi
                                          Hp   =            213
089

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        8783572
49                 X    =         2691032
65
 Y    =      -11448910
37  feet           Y    =        -3459612
59  meter
 Z    =       16900989
84                 Z    =         5164460
12
 XDOT =      16091
742154                 XDOT =        4833
624188
 YDOT =      18858
300995  feet/sec       YDOT =        5802
460707  meter/sec
 ZDOT =       4389
111463                 ZDOT =        1361
455000

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10751168
41                 X    =         3276956
13
 Y    =       -9520624
43  feet           Y    =        -2901886
33  meter
 Z    =       16960018
88                 Z    =         5169413
75
 XDOT =      11348
940954                 XDOT =        3459
157203
 YDOT =      20863
222072  feet/sec       YDOT =        6359
110088  meter/sec
 ZDOT =       4494
855879                 ZDOT =        1370
032072


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   18340
81190247  
00016717  00000-0  10270-3 0  9027
2 25544  51
6362 238
4613 0005282 119
7030 240
4648 15
54024615 25356


Satellite: ISS
Catalog Number: 25544
Epoch time:      18340
81190247   =   yrday
fracday
Element set:     902
Inclination:       51
6362  deg
RA of node:       238
4613  deg
Eccentricity:     
0005282     
Arg of perigee:   119
7030  deg
Mean anomaly:     240
4648  deg
Mean motion:   15
54024615  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2535
Checksum:              287


Coasting Arc #4 (Orbit 2549)
---------------------------------------

Vector Time (GMT): 2018/341/18:16:16
000
Vector Time (MET): N/A
Weight (LBS)     : 944383
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3753351
38                 A    =         6777650
26  meter
 Y    =        2046469
43  meter          E    =           
0019548
 Z    =       -5276301
32                 I    =           51
31146
 XDOT =      -4258
295222                 Wp   =          102
29133
 YDOT =      -6334
444103  meter/sec      RA   =          232
66058  deg
 ZDOT =        570
015386                 TA   =          173
19692
                                          MA   =          173
17034
                                          Ha   =            222
899  n
mi
                                          Hp   =            212
916

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12314144
96                 X    =        -3750326
83
 Y    =        6714138
57  feet           Y    =         2004514
40  meter
 Z    =      -17310699
88                 Z    =        -5294526
43
 XDOT =     -13970
784848                 XDOT =       -4189
914076
 YDOT =     -20782
296926  feet/sec       YDOT =       -6381
681045  meter/sec
 ZDOT =       1870
129220                 ZDOT =         549
495139

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13205790
66                 X    =        -4025124
99
 Y    =        4412727
36  feet           Y    =         1344999
30  meter
 Z    =      -17392903
24                 Z    =        -5301356
91
 XDOT =      -9701
135366                 XDOT =       -2956
906059
 YDOT =     -21992
673093  feet/sec       YDOT =       -6703
366759  meter/sec
 ZDOT =       1778
523652                 ZDOT =         542
094009


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   18341
77647790  
00016717  00000-0  10270-3 0  9034
2 25544  51
6379 233
6540 0005351 123
9440 236
2221 15
54063216 25506


Satellite: ISS
Catalog Number: 25544
Epoch time:      18341
77647790   =   yrday
fracday
Element set:     903
Inclination:       51
6379  deg
RA of node:       233
6540  deg
Eccentricity:     
0005351     
Arg of perigee:   123
9440  deg
Mean anomaly:     236
2221  deg
Mean motion:   15
54063216  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2550
Checksum:              294


Coasting Arc #5 (Orbit 2551)
---------------------------------------

Vector Time (GMT): 2018/341/20:20:00
000
Vector Time (MET): N/A
Weight (LBS)     : 944383
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1356542
79                 A    =         6785281
03  meter
 Y    =       -5854327
51  meter          E    =           
0017239
 Z    =        3138397
84                 I    =           51
34072
 XDOT =       5837
536993                 Wp   =           97
35527
 YDOT =       1243
914585  meter/sec      RA   =          232
25887  deg
 ZDOT =       4818
639360                 TA   =          299
00213
                                          MA   =          299
17479
                                          Ha   =            222
812  n
mi
                                          Hp   =            213
103

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -4450599
71                 X    =        -1306222
10
 Y    =      -19207111
26  feet           Y    =        -5869216
34  meter
 Z    =       10296580
83                 Z    =         3131929
65
 XDOT =      19152
024254                 XDOT =        5799
786657
 YDOT =       4081
084596  feet/sec       YDOT =        1308
982317  meter/sec
 ZDOT =      15809
184253                 ZDOT =        4846
904884

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11008101
41                 X    =        -3355269
31
 Y    =      -16374607
38  feet           Y    =        -4990980
33  meter
 Z    =       10268129
04                 Z    =         3129725
73
 XDOT =      18067
066274                 XDOT =        5506
841800
 YDOT =      -2101
176866  feet/sec       YDOT =        -640
438709  meter/sec
 ZDOT =      15936
190037                 ZDOT =        4857
350723


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   18341
90508618  
00016717  00000-0  10270-3 0  9045
2 25544  51
6397 233
0121 0005288 127
4481 232
7153 15
54093334 25529


Satellite: ISS
Catalog Number: 25544
Epoch time:      18341
90508618   =   yrday
fracday
Element set:     904
Inclination:       51
6397  deg
RA of node:       233
0121  deg
Eccentricity:     
0005288     
Arg of perigee:   127
4481  deg
Mean anomaly:     232
7153  deg
Mean motion:   15
54093334  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2552
Checksum:              298


Coasting Arc #6 (Orbit 2566)
---------------------------------------

Vector Time (GMT): 2018/342/20:20:00
000
Vector Time (MET): N/A
Weight (LBS)     : 964842
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =          94691
85                 A    =         6781572
29  meter
 Y    =        5217651
59  meter          E    =           
0012204
 Z    =       -4341277
48                 I    =           51
34895
 XDOT =      -6273
325437                 Wp   =           91
82009
 YDOT =      -2738
203767  meter/sec      RA   =          227
25408  deg
 ZDOT =      -3436
571458                 TA   =          143
15501
                                          MA   =          143
07109
                                          Ha   =            222
833  n
mi
                                          Hp   =            213
181

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =         310668
79                 X    =           57427
36
 Y    =       17118279
51  feet           Y    =         5218502
70  meter
 Z    =      -14243036
37                 Z    =        -4340907
34
 XDOT =     -20581
776368                 XDOT =       -6225
546653
 YDOT =      -8983
608160  feet/sec       YDOT =       -2808
088863  meter/sec
 ZDOT =     -11274
840743                 ZDOT =       -3466
929638

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        6693995
91                 X    =         2040329
95
 Y    =       15759243
32  feet           Y    =         4803417
37  meter
 Z    =      -14241936
74                 Z    =        -4340942
32
 XDOT =     -21225
149645                 XDOT =       -6469
425612
 YDOT =      -1270
709677  feet/sec       YDOT =        -387
312310  meter/sec
 ZDOT =     -11411
118210                 ZDOT =       -3478
108830


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   18342
86966091  
00016717  00000-0  10270-3 0  9055
2 25544  51
6395 228
2046 0005286 129
3479 230
8143 15
54053124 25672


Satellite: ISS
Catalog Number: 25544
Epoch time:      18342
86966091   =   yrday
fracday
Element set:     905
Inclination:       51
6395  deg
RA of node:       228
2046  deg
Eccentricity:     
0005286     
Arg of perigee:   129
3479  deg
Mean anomaly:     230
8143  deg
Mean motion:   15
54053124  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2567
Checksum:              321


Coasting Arc #7 (Orbit 2582)
---------------------------------------

Vector Time (GMT): 2018/343/20:20:00
000
Vector Time (MET): N/A
Weight (LBS)     : 964842
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1267538
87                 A    =         6778494
96  meter
 Y    =       -4317339
63  meter          E    =           
0010592
 Z    =        5064342
63                 I    =           51
36192
 XDOT =       6368
906666                 Wp   =          129
24249
 YDOT =       3912
662429  meter/sec      RA   =          222
24123  deg
 ZDOT =       1732
463214                 TA   =          303
90521
                                          MA   =          304
00590
                                          Ha   =            222
691  n
mi
                                          Hp   =            213
208

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        4158592
09                 X    =         1291122
37
 Y    =      -14164500
10  feet           Y    =        -4303033
91  meter
 Z    =       16615297
36                 Z    =         5070556
66
 XDOT =      20895
363077                 XDOT =        6316
265407
 YDOT =      12836
818994  feet/sec       YDOT =        3983
589414  meter/sec
 ZDOT =       5683
934428                 ZDOT =        1763
273911

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -1716774
70                 X    =         -523272
93
 Y    =      -14629914
47  feet           Y    =        -4459197
93  meter
 Z    =       16643717
88                 Z    =         5073005
21
 XDOT =      23124
695973                 XDOT =        7048
407333
 YDOT =       3943
552938  feet/sec       YDOT =        1201
994936  meter/sec
 ZDOT =       5822
146497                 ZDOT =        1774
590252


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   18343
89853652  
00016717  00000-0  10270-3 0  9068
2 25544  51
6390 223
0764 0005263 133
3493 226
8099 15
54093555 25838


Satellite: ISS
Catalog Number: 25544
Epoch time:      18343
89853652   =   yrday
fracday
Element set:     906
Inclination:       51
6390  deg
RA of node:       223
0764  deg
Eccentricity:     
0005263     
Arg of perigee:   133
3493  deg
Mean anomaly:     226
8099  deg
Mean motion:   15
54093555  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2583
Checksum:              330


Coasting Arc #8 (Orbit 2597)
---------------------------------------

Vector Time (GMT): 2018/344/20:20:00
000
Vector Time (MET): N/A
Weight (LBS)     : 964842
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2718015
25                 A    =         6777511
81  meter
 Y    =        3254776
09  meter          E    =           
0018951
 Z    =       -5303258
19                 I    =           51
38426
 XDOT =      -6010
622971                 Wp   =          102
64352
 YDOT =      -4736
812520  meter/sec      RA   =          217
22480  deg
 ZDOT =        169
872708                 TA   =          169
00477
                                          MA   =          168
96330
                                          Ha   =            222
705  n
mi
                                          Hp   =            213
175

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8917372
87                 X    =        -2728448
62
 Y    =       10678399
25  feet           Y    =         3224323
65  meter
 Z    =      -17399141
05                 Z    =        -5316486
33
 XDOT =     -19719
891636                 XDOT =       -5958
033038
 YDOT =     -15540
723492  feet/sec       YDOT =       -4803
733454  meter/sec
 ZDOT =        557
325156                 ZDOT =         140
802337

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -3784012
55                 X    =        -1153367
02
 Y    =       13309472
52  feet           Y    =         4056727
22  meter
 Z    =      -17459010
54                 Z    =        -5321506
41
 XDOT =     -23327
827667                 XDOT =       -7110
321873
 YDOT =      -6056
973135  feet/sec       YDOT =       -1846
165412  meter/sec
 ZDOT =        427
004578                 ZDOT =         130
150995


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   18344
86310787  
00016717  00000-0  10270-3 0  9074
2 25544  51
6394 218
2693 0005245 135
8469 224
3103 15
54078712 25982


Satellite: ISS
Catalog Number: 25544
Epoch time:      18344
86310787   =   yrday
fracday
Element set:     907
Inclination:       51
6394  deg
RA of node:       218
2693  deg
Eccentricity:     
0005245     
Arg of perigee:   135
8469  deg
Mean anomaly:     224
3103  deg
Mean motion:   15
54078712  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2598
Checksum:              330


Coasting Arc #9 (Orbit 2599)
---------------------------------------

Vector Time (GMT): 2018/344/23:07:30
000
Vector Time (MET): N/A
Weight (LBS)     : 964842
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4026447
72                 A    =         6787750
26  meter
 Y    =        5053662
03  meter          E    =           
0011736
 Z    =       -2067763
06                 I    =           51
42025
 XDOT =      -5021
962530                 Wp   =          138
14246
 YDOT =       1752
824000  meter/sec      RA   =          216
66441  deg
 ZDOT =      -5521
762911                 TA   =           64
80450
                                          MA   =           64
68286
                                          Ha   =            222
725  n
mi
                                          Hp   =            213
364

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13210130
30                 X    =         3979681
10
 Y    =       16580256
00  feet           Y    =         5098427
32  meter
 Z    =       -6783999
53                 Z    =        -2048316
96
 XDOT =     -16476
255020                 XDOT =       -5014
368042
 YDOT =       5750
734909  feet/sec       YDOT =        1696
708036  meter/sec
 ZDOT =     -18116
020049                 ZDOT =       -5546
139221

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       20573032
59                 X    =         6270660
33
 Y    =       -5228320
93  feet           Y    =        -1593592
22  meter
 Z    =       -6697019
59                 Z    =        -2041251
57
 XDOT =      -1896
465788                 XDOT =        -578
042772
 YDOT =      15769
672175  feet/sec       YDOT =        4806
596079  meter/sec
 ZDOT =     -18225
900447                 ZDOT =       -5555
254456


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   18344
99171686  
00016717  00000-0  10270-3 0  9082
2 25544  51
6383 217
6300 0005127 135
6696 224
4868 15
54062504 26002


Satellite: ISS
Catalog Number: 25544
Epoch time:      18344
99171686   =   yrday
fracday
Element set:     908
Inclination:       51
6383  deg
RA of node:       217
6300  deg
Eccentricity:     
0005127     
Arg of perigee:   135
6696  deg
Mean anomaly:     224
4868  deg
Mean motion:   15
54062504  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2600
Checksum:              318


Coasting Arc #10 (Orbit 2615)
---------------------------------------

Vector Time (GMT): 2018/345/23:07:30
000
Vector Time (MET): N/A
Weight (LBS)     : 964842
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2893834
18                 A    =         6784386
00  meter
 Y    =       -5046486
19  meter          E    =           
0016170
 Z    =        3481413
05                 I    =           51
43680
 XDOT =       6185
360329                 Wp   =          104
65154
 YDOT =       -415
646547  meter/sec      RA   =          211
67157  deg
 ZDOT =       4517
299786                 TA   =          296
40039
                                          MA   =          296
56628
                                          Ha   =            222
652  n
mi
                                          Hp   =            213
411

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9494206
62                 X    =        -2854098
72
 Y    =      -16556713
23  feet           Y    =        -5078625
25  meter
 Z    =       11421958
82                 Z    =         3467451
81
 XDOT =      20293
176931                 XDOT =        6167
605879
 YDOT =      -1363
669775  feet/sec       YDOT =        -346
577297  meter/sec
 ZDOT =      14820
537356                 ZDOT =        4547
302905

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -18994860
62                 X    =        -5789633
52
 Y    =        2208989
18  feet           Y    =          673299
90  meter
 Z    =       11359643
15                 Z    =         3462419
23
 XDOT =       6929
498496                 XDOT =        2112
111141
 YDOT =     -17689
437186  feet/sec       YDOT =       -5391
740454  meter/sec
 ZDOT =      14955
617284                 ZDOT =        4558
472148


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   18346
02058822  
00016717  00000-0  10270-3 0  9095
2 25544  51
6387 212
5011 0005061 138
5114 221
6424 15
54080889 26163


Satellite: ISS
Catalog Number: 25544
Epoch time:      18346
02058822   =   yrday
fracday
Element set:     909
Inclination:       51
6387  deg
RA of node:       212
5011  deg
Eccentricity:     
0005061     
Arg of perigee:   138
5114  deg
Mean anomaly:     221
6424  deg
Mean motion:   15
54080889  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2616
Checksum:              292


Coasting Arc #11 (Orbit 2630)
---------------------------------------

Vector Time (GMT): 2018/346/23:07:30
000
Vector Time (MET): N/A
Weight (LBS)     : 964842
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1423213
66                 A    =         6780679
92  meter
 Y    =        4801006
79  meter          E    =           
0012604
 Z    =       -4582521
64                 I    =           51
45237
 XDOT =      -6988
351670                 Wp   =           92
78765
 YDOT =       -810
741035  meter/sec      RA   =          206
67122  deg
 ZDOT =      -3027
616923                 TA   =          146
89125
                                          MA   =          146
81230
                                          Ha   =            222
631  n
mi
                                          Hp   =            213
490

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        4669336
15                 X    =         1391681
09
 Y    =       15751334
62  feet           Y    =         4816746
27  meter
 Z    =      -15034519
82                 Z    =        -4575684
33
 XDOT =     -22927
662960                 XDOT =       -6964
059823
 YDOT =      -2659
911533  feet/sec       YDOT =        -888
753540  meter/sec
 ZDOT =      -9933
126387                 ZDOT =       -3061
504899

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16378992
57                 X    =         4992316
93
 Y    =        1595530
43  feet           Y    =          486317
67  meter
 Z    =      -15004229
86                 Z    =        -4573289
26
 XDOT =     -11059
107256                 XDOT =       -3370
815892
 YDOT =      18925
515616  feet/sec       YDOT =        5768
497160  meter/sec
 ZDOT =     -10085
586814                 ZDOT =       -3074
086861


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   18346
98515610  
00016717  00000-0  10270-3 0  9105
2 25544  51
6380 207
6934 0005107 141
0061 219
1461 15
54059024 26313


Satellite: ISS
Catalog Number: 25544
Epoch time:      18346
98515610   =   yrday
fracday
Element set:     910
Inclination:       51
6380  deg
RA of node:       207
6934  deg
Eccentricity:     
0005107     
Arg of perigee:   141
0061  deg
Mean anomaly:     219
1461  deg
Mean motion:   15
54059024  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2631
Checksum:              282


Coasting Arc #12 (Orbit 2646)
---------------------------------------

Vector Time (GMT): 2018/347/23:07:30
000
Vector Time (MET): N/A
Weight (LBS)     : 964842
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         202615
62                 A    =         6778049
20  meter
 Y    =       -4359066
14  meter          E    =           
0009138
 Z    =        5182188
82                 I    =           51
47388
 XDOT =       7341
612063                 Wp   =          136
03812
 YDOT =       1841
682018  meter/sec      RA   =          201
66411  deg
 ZDOT =       1254
327711                 TA   =          301
85504
                                          MA   =          301
94395
                                          Ha   =            222
513  n
mi
                                          Hp   =            213
544

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =         664749
41                 X    =          226172
58
 Y    =      -14301398
11  feet           Y    =        -4356669
04  meter
 Z    =       17001931
81                 Z    =         5183229
93
 XDOT =      24086
653751                 XDOT =        7314
379368
 YDOT =       6042
263838  feet/sec       YDOT =        1923
628663  meter/sec
 ZDOT =       4115
248395                 ZDOT =        1289
924637

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13110478
58                 X    =        -3996073
87
 Y    =       -5736985
04  feet           Y    =        -1748633
04  meter
 Z    =       17007054
98                 Z    =         5183750
36
 XDOT =      13995
098880                 XDOT =        4265
706139
 YDOT =     -19232
710899  feet/sec       YDOT =       -5862
130282  meter/sec
 ZDOT =       4275
320470                 ZDOT =        1303
117679


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   18348
01402507  
00016717  00000-0  10270-3 0  9112
2 25544  51
6379 202
5650 0005022 145
0557 215
0926 15
54081201 26470


Satellite: ISS
Catalog Number: 25544
Epoch time:      18348
01402507   =   yrday
fracday
Element set:     911
Inclination:       51
6379  deg
RA of node:       202
5650  deg
Eccentricity:     
0005022     
Arg of perigee:   145
0557  deg
Mean anomaly:     215
0926  deg
Mean motion:   15
54081201  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2647
Checksum:              276


Coasting Arc #13 (Orbit 2649)
---------------------------------------

Vector Time (GMT): 2018/348/03:56:00
000
Vector Time (MET): N/A
Weight (LBS)     : 964842
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4426187
87                 A    =         6780342
02  meter
 Y    =       -2251526
75  meter          E    =           
0010362
 Z    =        4607347
87                 I    =           51
48582
 XDOT =       5412
980736                 Wp   =           92
62871
 YDOT =       4560
413770  meter/sec      RA   =          200
63132  deg
 ZDOT =      -2966
249257                 TA   =           27
00037
                                          MA   =           26
94650
                                          Ha   =            222
364  n
mi
                                          Hp   =            213
563

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14521613
76                 X    =         4428656
09
 Y    =       -7386898
79  feet           Y    =        -2202016
58  meter
 Z    =       15115970
70                 Z    =         4628854
54
 XDOT =      17759
123148                 XDOT =        5375
991052
 YDOT =      14961
987434  feet/sec       YDOT =        4620
738883  meter/sec
 ZDOT =      -9731
788902                 ZDOT =       -2940
044427

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15848811
72                 X    =        -4830717
81
 Y    =       -3363821
04  feet           Y    =        -1025292
65  meter
 Z    =       15213020
26                 Z    =         4636928
57
 XDOT =      -4640
302490                 XDOT =       -1414
364199
 YDOT =     -21696
091524  feet/sec       YDOT =       -6612
968697  meter/sec
 ZDOT =      -9614
267447                 ZDOT =       -2930
428718


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   18348
20693851  
00016717  00000-0  10270-3 0  9128
2 25544  51
6358 201
6038 0004863 143
7427 216
4056 15
54076193 26507


Satellite: ISS
Catalog Number: 25544
Epoch time:      18348
20693851   =   yrday
fracday
Element set:     912
Inclination:       51
6358  deg
RA of node:       201
6038  deg
Eccentricity:     
0004863     
Arg of perigee:   143
7427  deg
Mean anomaly:     216
4056  deg
Mean motion:   15
54076193  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2650
Checksum:              309


Coasting Arc #14 (Orbit 2664)
---------------------------------------

Vector Time (GMT): 2018/349/03:56:00
000
Vector Time (MET): N/A
Weight (LBS)     : 964842
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5617552
87                 A    =         6784056
40  meter
 Y    =        1366165
13  meter          E    =           
0009273
 Z    =       -3561128
67                 I    =           51
53046
 XDOT =      -3985
194444                 Wp   =          120
65431
 YDOT =      -4789
531643  meter/sec      RA   =          195
63465  deg
 ZDOT =       4453
108514                 TA   =          197
28920
                                          MA   =          197
32080
                                          Ha   =            222
463  n
mi
                                          Hp   =            213
552

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -18430291
58                 X    =        -5615114
13
 Y    =        4482169
05  feet           Y    =         1303359
60  meter
 Z    =      -11683493
00                 Z    =        -3588410
77
 XDOT =     -13074
784922                 XDOT =       -3952
971217
 YDOT =     -15713
686492  feet/sec       YDOT =       -4833
916965  meter/sec
 ZDOT =      14609
936070                 ZDOT =        4433
827791

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17204542
83                 X    =         5243944
65
 Y    =        7802594
59  feet           Y    =         2378230
83  meter
 Z    =      -11806469
40                 Z    =        -3598611
87
 XDOT =       1232
922732                 XDOT =         375
794849
 YDOT =      19237
973880  feet/sec       YDOT =        5863
734439  meter/sec
 ZDOT =      14523
594101                 ZDOT =        4426
791482


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   18349
17150135  
00016717  00000-0  10270-3 0  9139
2 25544  51
6368 196
7959 0004813 145
6510 214
4955 15
54056379 26659


Satellite: ISS
Catalog Number: 25544
Epoch time:      18349
17150135   =   yrday
fracday
Element set:     913
Inclination:       51
6368  deg
RA of node:       196
7959  deg
Eccentricity:     
0004813     
Arg of perigee:   145
6510  deg
Mean anomaly:     214
4955  deg
Mean motion:   15
54056379  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2665
Checksum:              332


Coasting Arc #15 (Orbit 2680)
---------------------------------------

Vector Time (GMT): 2018/350/03:56:00
000
Vector Time (MET): N/A
Weight (LBS)     : 964842
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6419248
99                 A    =         6787495
78  meter
 Y    =        -501532
16  meter          E    =           
0017779
 Z    =        2116714
06                 I    =           51
57417
 XDOT =       2205
871383                 Wp   =          119
79151
 YDOT =       4863
598084  meter/sec      RA   =          190
65012  deg
 ZDOT =      -5511
173928                 TA   =           36
71527
                                          MA   =           36
59360
                                          Ha   =            222
281  n
mi
                                          Hp   =            213
696

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       21060528
19                 X    =         6414098
27
 Y    =       -1645446
72  feet           Y    =         -429776
57  meter
 Z    =        6944599
92                 Z    =         2147884
07
 XDOT =       7237
110835                 XDOT =        2178
091757
 YDOT =      15956
686626  feet/sec       YDOT =        4888
110654  meter/sec
 ZDOT =     -18081
279292                 ZDOT =       -5500
525745

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17746130
58                 X    =        -5409020
60
 Y    =      -11373576
55  feet           Y    =        -3466666
13  meter
 Z    =        7085013
51                 Z    =         2159512
12
 XDOT =       2936
320096                 XDOT =         894
990365
 YDOT =     -15867
683705  feet/sec       YDOT =       -4836
469993  meter/sec
 ZDOT =     -18033
804280                 ZDOT =       -5496
703545


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   18350
20036698  
00016717  00000-0  10270-3 0  9143
2 25544  51
6366 191
6669 0004722 149
5449 210
5979 15
54080273 26813


Satellite: ISS
Catalog Number: 25544
Epoch time:      18350
20036698   =   yrday
fracday
Element set:     914
Inclination:       51
6366  deg
RA of node:       191
6669  deg
Eccentricity:     
0004722     
Arg of perigee:   149
5449  deg
Mean anomaly:     210
5979  deg
Mean motion:   15
54080273  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2681
Checksum:              330


Coasting Arc #16 (Orbit 2695)
---------------------------------------

Vector Time (GMT): 2018/351/03:56:00
000
Vector Time (MET): N/A
Weight (LBS)     : 964842
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6763638
83                 A    =         6789307
96  meter
 Y    =        -280521
46  meter          E    =           
0010115
 Z    =        -492011
47                 I    =           51
61300
 XDOT =       -229
262934                 Wp   =           67
83505
 YDOT =      -4785
589573  meter/sec      RA   =          185
67587  deg
 ZDOT =       5982
490200                 TA   =          286
85859
                                          MA   =          286
96949
                                          Ha   =            222
273  n
mi
                                          Hp   =            213
803

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -22190416
11                 X    =        -6757609
33
 Y    =        -920346
01  feet           Y    =         -356123
43  meter
 Z    =       -1614210
86                 Z    =         -524852
43
 XDOT =       -752
174980                 XDOT =        -204
792023
 YDOT =     -15700
753193  feet/sec       YDOT =       -4788
016870  meter/sec
 ZDOT =      19627
592519                 ZDOT =        5981
435674

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17367034
07                 X    =         5293471
98
 Y    =       13825644
48  feet           Y    =         4214056
44  meter
 Z    =       -1762090
50                 Z    =         -537085
18
 XDOT =      -7538
947700                 XDOT =       -2297
871259
 YDOT =      11931
837075  feet/sec       YDOT =        3636
823941  meter/sec
 ZDOT =      19623
309681                 ZDOT =        5981
184791


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   18351
16492751  
00016717  00000-0  10270-3 0  9156
2 25544  51
6364 186
8594 0004819 153
9816 206
1580 15
54091686 26963


Satellite: ISS
Catalog Number: 25544
Epoch time:      18351
16492751   =   yrday
fracday
Element set:     915
Inclination:       51
6364  deg
RA of node:       186
8594  deg
Eccentricity:     
0004819     
Arg of perigee:   153
9816  deg
Mean anomaly:     206
1580  deg
Mean motion:   15
54091686  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2696
Checksum:              343


Coasting Arc #17 (Orbit 2711)
---------------------------------------

Vector Time (GMT): 2018/352/03:56:00
000
Vector Time (MET): N/A
Weight (LBS)     : 964842
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6586655
76                 A    =         6788853
14  meter
 Y    =        1052735
29  meter          E    =           
0013726
 Z    =       -1227867
01                 I    =           51
64591
 XDOT =      -1820
235464                 Wp   =          147
75932
 YDOT =       4609
765559  meter/sec      RA   =          180
70515  deg
 ZDOT =      -5853
529330                 TA   =           45
58845
                                          MA   =           45
47618
                                          Ha   =            222
215  n
mi
                                          Hp   =            213
950

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       21609762
98                 X    =         6580358
62
 Y    =        3453855
93  feet           Y    =         1126356
73  meter
 Z    =       -4028435
07                 Z    =        -1195886
29
 XDOT =      -5971
901128                 XDOT =       -1843
214291
 YDOT =      15123
902751  feet/sec       YDOT =        4589
282341  meter/sec
 ZDOT =     -19204
492553                 ZDOT =       -5862
426967

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15699619
01                 X    =        -4785243
87
 Y    =      -15283062
18  feet           Y    =        -4658277
35  meter
 Z    =       -3884486
97                 Z    =        -1183991
63
 XDOT =      12371
589053                 XDOT =        3770
860343
 YDOT =      -7853
182063  feet/sec       YDOT =       -2393
649893  meter/sec
 ZDOT =     -19245
020003                 ZDOT =       -5865
882097


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   18352
19378948  
00016717  00000-0  10270-3 0  9162
2 25544  51
6379 181
7302 0004618 157
9363 202
1989 15
54087510 27127


Satellite: ISS
Catalog Number: 25544
Epoch time:      18352
19378948   =   yrday
fracday
Element set:     916
Inclination:       51
6379  deg
RA of node:       181
7302  deg
Eccentricity:     
0004618     
Arg of perigee:   157
9363  deg
Mean anomaly:     202
1989  deg
Mean motion:   15
54087510  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2712
Checksum:              333


Coasting Arc #18 (Orbit 2727)
---------------------------------------

Vector Time (GMT): 2018/353/03:56:00
000
Vector Time (MET): N/A
Weight (LBS)     : 964842
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5929321
83                 A    =         6786215
31  meter
 Y    =       -1762434
54  meter          E    =           
0014844
 Z    =        2781043
35                 I    =           51
66965
 XDOT =       3704
915686                 Wp   =           97
64308
 YDOT =      -4338
829853  meter/sec      RA   =          175
73288  deg
 ZDOT =       5124
040806                 TA   =          293
87250
                                          MA   =          294
02797
                                          Ha   =            222
141  n
mi
                                          Hp   =            214
041

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -19453155
60                 X    =        -5922682
08
 Y    =       -5782265
55  feet           Y    =        -1828703
46  meter
 Z    =        9124157
97                 Z    =         2752256
45
 XDOT =      12155
235189                 XDOT =        3728
268218
 YDOT =     -14235
006079  feet/sec       YDOT =       -4297
268791  meter/sec
 ZDOT =      16811
157500                 ZDOT =        5142
094509

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12896419
53                 X    =         3930828
67
 Y    =       15744484
04  feet           Y    =         4798918
74  meter
 Z    =        8994648
50                 Z    =         2741568
86
 XDOT =     -16810
668693                 XDOT =       -5123
891818
 YDOT =       4070
770262  feet/sec       YDOT =        1240
770776  meter/sec
 ZDOT =      16892
913499                 ZDOT =        5148
960034


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   18353
22264884  
00016717  00000-0  10270-3 0  9171
2 25544  51
6371 176
6020 0004669 161
4900 198
6423 15
54104891 27283


Satellite: ISS
Catalog Number: 25544
Epoch time:      18353
22264884   =   yrday
fracday
Element set:     917
Inclination:       51
6371  deg
RA of node:       176
6020  deg
Eccentricity:     
0004669     
Arg of perigee:   161
4900  deg
Mean anomaly:     198
6423  deg
Mean motion:   15
54104891  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2728
Checksum:              318


Coasting Arc #19 (Orbit 2741)
---------------------------------------

Vector Time (GMT): 2018/354/01:40:30
000
Vector Time (MET): N/A
Weight (LBS)     : 949610
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3595200
32                 A    =         6779931
22  meter
 Y    =       -3239560
97  meter          E    =           
0011424
 Z    =        4745005
83                 I    =           51
67692
 XDOT =       6441
332854                 Wp   =          135
40000
 YDOT =      -3162
215924  meter/sec      RA   =          171
21792  deg
 ZDOT =       2709
618862                 TA   =          287
77540
                                          MA   =          287
90003
                                          Ha   =            222
087  n
mi
                                          Hp   =            214
128

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11795276
64                 X    =        -3581756
39
 Y    =      -10628480
88  feet           Y    =        -3279690
35  meter
 Z    =       15567604
43                 Z    =         4727573
72
 XDOT =      21132
981806                 XDOT =        6463
052881
 YDOT =     -10374
724161  feet/sec       YDOT =       -3090
063316  meter/sec
 ZDOT =       8889
825662                 ZDOT =        2740
961332

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5174670
69                 X    =        -1577239
63
 Y    =       15091230
09  feet           Y    =         4599806
93  meter
 Z    =       15489384
18                 Z    =         4721164
30
 XDOT =     -16640
694651                 XDOT =       -5072
083730
 YDOT =     -15015
921114  feet/sec       YDOT =       -4576
852755  meter/sec
 ZDOT =       9031
352313                 ZDOT =        2752
756185


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   18354
12290030  
00016717  00000-0  10270-3 0  9184
2 25544  51
6354 172
1147 0004640 166
0108 194
1173 15
54107206 27427


Satellite: ISS
Catalog Number: 25544
Epoch time:      18354
12290030   =   yrday
fracday
Element set:     918
Inclination:       51
6354  deg
RA of node:       172
1147  deg
Eccentricity:     
0004640     
Arg of perigee:   166
0108  deg
Mean anomaly:     194
1173  deg
Mean motion:   15
54107206  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2742
Checksum:              275
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